IP Library Granted Patent US 11,396,063
Granted Patent B2
US 11,396,063 · App. 16/827,159 · Granted Jul 26, 2022

Systems and methods for in process heating for direct energy deposition applications

Inventors: Rudy Pitera (Woodbury, MN); Scott Wigen (Eagan, MN); Paul Robert Johnson (Prior Lake, MN); Ryan Philip Chou (Richfield, MN)
Assignee: Rosemount Aerospace Inc.
B23K26/342B23K13/01B23K26/1464B23K26/702B33Y10/00B33Y30/00H05B6/06H05B6/101
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Quick Facts
Patent No.
US 11,396,063
App. No.
16/827,159
Granted
Jul 26, 2022
Kind
B2
Abstract

A system used to additively manufacture an object layer-by-layer using direct energy deposition (DED) includes a base where the object is formed, a depositor configured to deposit material layer-by-layer on the base or a previously deposited layer of the object, an energy source configured to selectively direct an energized beam at the material to fuse a new layer of the material to a previously formed layer, and a heating element in contact with at least a portion of the base and configured to supply heat to the base.

Claims (29)

1. A system used to additively manufacture an object layer-by-layer using direct energy deposition (DED), the system comprising:

a base having a first surface where the object is formed, and a second surface disposed on a side of the base opposite the first surface;

a depositor configured to deposit material layer-by-layer on the first surface of the base or a previously deposited layer of the object;

an energy source configured to selectively direct an energized beam at the material to fuse a new layer of the material to a previously formed layer; and

a heating element in direct physical contact with at least a portion of the second surface of the base and configured to conductively supply heat to the base.

2. The system of claim 1 , wherein the heating element comprises a plurality of tubular heating elements.

3. The system of claim 1 , wherein the base includes a tubular passageway.

4. The system of claim 3 , wherein the heating element comprises a plurality of tubular heating elements configured and arranged to fit within the tubular passageway and extend along a length of the tubular passageway.

5. The system of claim 1 , wherein a temperature of the base is 100 to 200 degrees Celsius above ambient temperature.

6. The system of claim 1 , wherein a temperature of the base is within 100 to 200 degrees Celsius of a melting temperature of the material.

7. A system used for direct energy deposition of layers of a material to repair a pre-existing component using direct energy deposition (DED), the system comprising:

a depositor configured to deposit material layer-by-layer on the pre-existing component or a previously deposited layer of material on the pre-existing component;

an energy source configured to selectively direct an energized beam at the material to fuse a new layer of the material to the pre-existing component or to a previously formed layer on the pre-existing component; and

a heating element extending through passageways within the pre-existing component and configured to supply heat to the pre-existing component, the heating element including heat tubing configured to circulate a heated fluid, and a heat-controlled bath apparatus connected to the tubing.

8. The system of claim 7 , wherein a temperature of the pre-existing component is 100 to 200 degrees Celsius above ambient temperature.

9. The system of claim 7 , wherein a temperature of the pre-exiting component is within 100 to 200 degrees Celsius of a melting temperature of the material.

10. A method of depositing layers onto a base using direct energy deposition (DED), the method comprising:

conductively heating the base using a heating element in direct physical contact with a first surface of the base;

depositing a layer of material on a second surface of the base or on a previously deposited layer;

providing energy to the material after each layer is deposited, the energy being provided by an energy source that forms an energized beam directed at the material;

melting the material; and

allowing the material to solidify to bond the material to the second surface of the base or the previously deposited layer;

wherein the first surface is opposite the second surface.

11. The method of claim 10 , wherein the heating step is carried out by a plurality of heating elements configured and arranged to fit within and/or extend along a length of the base.

12. The method of claim 10 , wherein the heating step includes heating the base to 100 to 200 degrees Celsius greater than ambient temperature prior to the depositing step.

13. The method of claim 10 , wherein the heating step includes heating the base to a temperature such that a difference between the temperature of the base and a melting temperature of the material being applied to the base is reduced to 100 to 200 degrees Celsius.

14. The method of claim 10 , wherein the energy source is selected from a group consisting of a laser and an electron beam.

15. The method of claim 10 , further comprising:

monitoring heat of the base to determine a temperature of the base prior to the depositing step.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 8, 2020
From: PITERA, RUDY; WIGEN, SCOTT; JOHNSON, PAUL ROBERT; CHOU, RYAN PHILIP
To: ROSEMOUNT AEROSPACE INC.
Reel/Frame 054645/0067 →
Continuity (1)
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